US8956136B2ActiveUtilityA1

Method of and device for cooling blown film during the production of blown film

90
Assignee: ZIMMERMANN RICHARDPriority: Apr 17, 2007Filed: Apr 17, 2008Granted: Feb 17, 2015
Est. expiryApr 17, 2027(~0.8 yrs left)· nominal 20-yr term from priority
B29C 48/10B29C 2948/92704B29C 2948/92152B29C 2948/926B29C 2948/92428B29C 48/908B29C 48/92B29C 2948/92923B29C 2948/92647B29C 48/903B29C 48/906B29C 48/0018B29L 2023/001B29C 48/0019B29C 48/89B29C 48/912B29C 48/885B29C 2947/92152B29C 2947/926B29C 47/92B29C 47/0059B29C 47/0026B29C 2947/92647B29C 47/883B29C 47/8835B29C 47/0057B29C 2947/92704B29C 47/903B29C 2947/92923B29C 2947/92428
90
PatentIndex Score
26
Cited by
12
References
15
Claims

Abstract

A method of cooling blown film consisting of thermoplastic plastics during the production of blown film by means of a blown film extruder with a film blowing head which comprises an annular nozzle from which the blown film emerges and is guided away in an extraction direction, wherein at least two cooling gas flows are made to approach the blown film from the outside in at least two blowing-out planes located at a distance from the annular nozzle, wherein at least one cooling gas flow K G is blown out in the direction opposed to the extraction direction of the blown film and wherein at least one cooling gas flow K A is blown out in the extraction direction of the blown film, and wherein, at least one of the cooling gas flows K G , K A can be controlled around their circumference in sectors, at least in respect of its volume flow or temperature.

Claims

exact text as granted — not AI-modified
The invention claimed is: 
     
       1. A device for cooling blown film comprising thermoplastic plastics during the production of blown film for being arranged at a blown film extruder with a film blowing head, the film blowing head comprising:
 an annular nozzle from which the blown film is guided away in an extraction direction, and further comprising 
 at least three annular cooling gas nozzles arranged at a distance from the annular nozzle thereby forming at least three blowing-out planes, wherein 
 at least one of the at least three annular cooling gas nozzles is directed against the extraction direction of the blown film, 
 at least one of the at least three annular cooling gas nozzles is directed in a radial direction toward the blown film, and 
 at least one of the at least three annular cooling gas nozzles is directed in the extraction direction of the blown film, and wherein 
 the at least one annular cooling gas nozzle directed in a radial direction toward the blown film is arranged between the at least one annular cooling gas nozzle directed against the extraction direction of the blown film and the at least one annular cooling gas nozzle directed in the extraction direction of the blown film, wherein 
 the at least one annular cooling gas nozzle directed against the extraction direction of the blown film and the at least one annular cooling gas nozzle directed in the extraction direction of the blown film provide a common cooling ring and are fed from a common annular chamber, wherein 
 on the inside of the annular chamber an annular exit gap is provided, said annular exit gap being divided into channels for supplying all of the at least three annular cooling gas nozzles, 
 further comprising at least one variable controlling means, said at least one variable controlling means selected from the group consisting of means for circumferentially variably controlling in sectors the volume flow of said annular cooling gas nozzles and means for circumferentially variably controlling in sectors the temperature of the cooling gas flow of said annular cooling gas nozzles, wherein 
 said annular exit gap being provided with radial channels, and wherein 
 the variable controlling means has independently controlled setting elements provided in the annular chamber or in the annular exit gap so as to vary the free passage cross-sections of the radial channels or the temperature in sectors. 
 
     
     
       2. A device according to  claim 1 , further comprising at least two annular cooling gas nozzles directed in the extraction direction of the blown film and at least two annular cooling gas nozzles directed opposed to the extraction direction of the blown film, wherein the annular exit gap supplies all of the at least two annular cooling gas nozzles directed in the extraction direction of the blown film and all of the at least two annular cooling gas nozzles directed opposed to the extraction direction. 
     
     
       3. A device according to  claim 1 , further comprising a sucking-off device for the cooling gas distributed around the circumference and between the annular nozzle of the film blowing head and the at least one annular cooling gas nozzle directed against the extraction direction of the blown film. 
     
     
       4. A device according to  claim 1 , further comprising an annular deflection plate is arranged above the film blowing head. 
     
     
       5. A device according to  claim 1 , further comprising thermal insulation means arranged on the film blowing head. 
     
     
       6. A device for cooling blown film comprising thermoplastic plastics during the production of blown film for being arranged at a blown film extruder with a film blowing head, the film blowing head comprising:
 an annular nozzle from which the blown film is guided away in an extraction direction, and further comprising 
 at least three annular cooling gas nozzles arranged at a distance from the annular nozzle thereby forming at least three blowing-out planes, wherein 
 at least one of the at least three annular cooling gas nozzles is directed against the extraction direction of the blown film, 
 at least one of the at least three annular cooling gas nozzles is directed in a radial direction toward the blown film, and 
 at least one of the at least three annular cooling gas nozzles is directed in the extraction direction of the blown film, and wherein 
 the at least one annular cooling gas nozzle directed in a radial direction toward the blown film is arranged between the at least one annular cooling gas nozzle directed against the extraction direction of the blown film and the at least one annular cooling gas nozzle directed in the extraction direction of the blown film, wherein 
 the at least one annular cooling gas nozzle directed against the extraction direction of the blown film and the at least one annular cooling gas nozzle directed in the extraction direction of the blown film provide a common cooling ring and are fed from a common annular chamber, 
 wherein on the inside of the annular chamber an annular exit gap is provided, said annular exit gap being divided into channels for supplying all of the at least three annular cooling gas nozzles, 
 further comprising only one variable controlling means, said only one variable controlling means selected from the group consisting of means for circumferentially variably controlling in sectors the volume flow of said annular cooling gas nozzles and means for circumferentially variably controlling in sectors the temperature of the cooling gas flow of said annular cooling gas nozzles, 
 wherein said annular exit gap being provided with radial channels, and 
 wherein the variable controlling means has independently controlled setting elements provided in the annular chamber so as to vary the free passage cross-sections of the radial channels or the temperature in sectors. 
 
     
     
       7. A cooling ring for use with a blown film extruder that is adapted to move blown film in an extraction direction, the cooling ring comprising:
 an annular housing defining an annular chamber having an annular exit gap; 
 a first annular cooling gas nozzle that communicates with the annular exit gap and is adapted to direct a flow of cooling gas from the annular chamber to the blown film in a direction that is against the extraction direction of the blown film; 
 a second annular cooling gas nozzle that communicates with the annular exit gap and is adapted to direct a flow of cooling gas to the blown film in a direction that is radial to the extraction direction of the blown film; 
 a third annular cooling gas nozzle that communicates with the annular exit gap and is adapted to direct a flow of cooling gas from the annular chamber to the blown film in the extraction direction of the blown film, wherein 
 the second annular cooling gas nozzle is arranged between the first annular cooling gas nozzle and the third annular cooling gas nozzle. 
 
     
     
       8. The cooling ring defined in  claim 7  further including a means for circumferentially variably controlling in sectors a volume flow of the annular cooling gas nozzles. 
     
     
       9. The cooling ring defined in  claim 7  further including a means for circumferentially variably controlling in sectors a temperature of the cooling gas flow of the annular cooling gas nozzles. 
     
     
       10. The cooling ring defined in  claim 7  further wherein the annular exit gap being provided with radial channels. 
     
     
       11. The cooling ring defined in  claim 10  further including a variable controlling means having independently controlled setting elements provided in the annular chamber or in the annular exit gap so as to vary in sectors either volume flow of the annular cooling gas nozzles or temperature of the cooling gas flow of the annular cooling gas nozzles. 
     
     
       12. The cooling ring defined in  claim 7  further including a fourth annular cooling gas nozzle that communicates with the annular exit gap and is adapted to direct a flow of cooling gas from the annular chamber to the blown film in the extraction direction of the blown film. 
     
     
       13. The cooling ring defined in  claim 7  further including a cooling gas blower that communicates through a plurality of individual supply lines with the second annular cooling gas nozzle. 
     
     
       14. The cooling ring defined in  claim 13  further including individual control elements provided in each of the individual supply lines. 
     
     
       15. The cooling ring defined in  claim 13  further including individual heating elements provided in each of the individual supply lines.

Cited by (0)

No later patents cite this yet.

References (0)

No backward citations on record.